Free Vibration Analysis of Delaminated Composite Plate Using 3D Degenerated Element-Reference-Cited by-同舟云学术

Free Vibration Analysis of Delaminated Composite Plate Using 3D Degenerated Element

Published:2019-09 Issue:5 Volume:32 Page:04019070
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Tiwari Pratik¹^ORCID,Barman Swarup K.²^ORCID,Maiti Dipak K.³,Maity Damodar⁴

Affiliation:

1. Research Scholar, Dept. of Aerospace Engineering, Indian Institute of Technology Kharagpur, West Bengal 721302, India (corresponding author). ORCID: .

2. Research Scholar, Dept. of Aerospace Engineering, Indian Institute of Technology Kharagpur, West Bengal 721302, India. ORCID: .

3. Professor, Dept. of Aerospace Engineering, Indian Institute of Technology Kharagpur, West Bengal 721302, India.

4. Professor, Dept. of Civil Engineering, Indian Institute of Technology Kharagpur, West Bengal 721302, India.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0001053

Reference35 articles.

1. Analysis of thick and thin shell structures by curved finite elements

2. A piezolaminated composite degenerated shell finite element for active control of structures with distributed piezosensors and actuators

3. Modeling of delamination in composite laminates using a layer-wise plate theory;Barbero E.;Int. J. Numer. Methods Eng.,1991

4. New higher order plate theory in modeling delamination buckling of composite laminates

5. Higher-Order Zig-Zag Theory for Laminated Composites With Multiple Delaminations

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